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CN102765198A - Vacuum assisted molding system of composite and molding method of composite - Google Patents

Vacuum assisted molding system of composite and molding method of composite Download PDF

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CN102765198A
CN102765198A CN2012102425007A CN201210242500A CN102765198A CN 102765198 A CN102765198 A CN 102765198A CN 2012102425007 A CN2012102425007 A CN 2012102425007A CN 201210242500 A CN201210242500 A CN 201210242500A CN 102765198 A CN102765198 A CN 102765198A
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vacuum bag
vacuum
mold
prepreg
molding
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彭超义
李仕通
杨明敏
肖加余
曾竟成
邢素丽
尹昌平
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National University of Defense Technology
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Abstract

本发明公开了一种复合材料真空辅助模压成型系统,包括一开放式成型模具,该模具包括上模和下模,下模上密封连接有真空袋压系统;模具外侧连接有模压加热系统。本发明还公开一种真空辅助模压成型复合材料制品的方法:先制备开放式成型模具,并将预浸料置于下模上,将隔离膜、脱模布、透气毡依次铺放,密封连接真空袋膜,使形成的真空袋压腔与真空泵相连通;上模和下模连接至模压加热系统;在保持真空袋压的条件下,将上模和下模进行合模,通过模压加热系统对预浸料进行合模加压,同时对上、下模进行加热,达到固化温度后进行固化处理,固化反应结束后成型得到复合材料制品。本发明的工艺成本低、通用性强、辅材消耗少,能改善产品的使用性能。

The invention discloses a composite material vacuum auxiliary molding system, which comprises an open molding mould. The mold includes an upper mold and a lower mold. The upper mold is sealed and connected with a vacuum bag pressure system; the outer side of the mold is connected with a molding heating system. The invention also discloses a method for vacuum-assisted molding of composite material products: first prepare an open molding mold, place the prepreg on the lower mold, place the isolation film, release cloth, and air felt in sequence, and seal and connect Vacuum bag film, so that the formed vacuum bag pressure chamber is connected with the vacuum pump; the upper mold and the lower mold are connected to the molding heating system; under the condition of maintaining the vacuum bag pressure, the upper mold and the lower mold are closed, and the mold is passed through the molding heating system. Clamp and pressurize the prepreg, heat the upper and lower molds at the same time, and perform curing treatment after reaching the curing temperature. After the curing reaction is completed, the composite material product is formed. The process of the invention has low cost, strong versatility, less consumption of auxiliary materials, and can improve the use performance of products.

Description

复合材料真空辅助模压成型系统及成型方法Composite material vacuum assisted compression molding system and molding method

技术领域 technical field

本发明属于复合材料成型工艺技术领域,尤其涉及用于提高预浸料模压成型制品内部和表面质量的成型系统及其成型方法。 The invention belongs to the technical field of composite material forming technology, and in particular relates to a forming system and a forming method for improving the internal and surface quality of prepreg molded products.

背景技术 Background technique

真空辅助模压成型系统是一种利用真空负压和模压共同作用将预浸料制备成型的低成本制造技术。抽真空,使成型系统内部形成负压,是提高制品内部质量的关键因素;施加外部压力,是提高制品中增强体含量和树脂致密度的关键因素。因此,抽真空与模压相结合的工艺是提高复合材料制品使用性能的一种重要技术。 Vacuum-assisted compression molding system is a low-cost manufacturing technology that uses the combined action of vacuum negative pressure and molding pressure to prepare prepregs. Vacuumizing to form a negative pressure inside the molding system is a key factor to improve the internal quality of the product; applying external pressure is a key factor to increase the reinforcement content and resin density in the product. Therefore, the process of combining vacuum pumping and molding is an important technology to improve the performance of composite products.

传统的利用真空负压制备成型的真空袋压工艺能够获得内部和表观质量较好的复合材料制品,但树脂含量偏高,力学性能偏低。传统模压工艺可以通过加压的途径获得力学性能相对较好的制品,但模压压力越大,复合材料内部结构受损的风险越高;压力较小,则内部空隙和缺陷越多。传统热压罐工艺能够成型内部质量和表观质量具佳的制品,但该方法设备成本与制造成本均较高,且成型压力偏低,安全风险较高。 The traditional vacuum bagging process using vacuum negative pressure to prepare and form can obtain composite products with better internal and apparent quality, but the resin content is relatively high and the mechanical properties are relatively low. The traditional molding process can obtain products with relatively good mechanical properties through pressurization, but the greater the molding pressure, the higher the risk of damage to the internal structure of the composite material; the lower the pressure, the more internal voids and defects. The traditional autoclave process can form products with good internal and external quality, but this method has high equipment costs and manufacturing costs, and the forming pressure is relatively low, resulting in high safety risks.

针对通常SMC/BMC模压成型产品表面出现的由于空气集聚造成的砂眼,中国专利200720187263.3设计了一种模压成型用的真空辅助成型模具,改善了制品存在的表面缺陷问题,提高了模压产品的表面精度。但该模具不仅需要设计真空孔,而且需要设计精度较高的密封槽保证模具合模后的密封效果,模具通用性偏低,工艺成本偏高。 Aiming at the trachoma caused by air accumulation on the surface of SMC/BMC compression molding products, Chinese patent 200720187263.3 designed a vacuum-assisted molding mold for compression molding, which improved the surface defects of products and improved the surface accuracy of molding products. . However, this mold not only needs to design vacuum holes, but also needs to design high-precision sealing grooves to ensure the sealing effect after the mold is closed. The versatility of the mold is relatively low, and the process cost is relatively high.

发明内容 Contents of the invention

为解决现有技术中存在的问题,本发明提出了一种结构简单、操作方便、成本低、产品质量高的复合材料真空辅助模压成型系统,还提供一种工艺成本低、通用性强、辅材消耗少、工艺门槛低、经济性好、能改善产品的使用性能的真空辅助模压成型复合材料制品的方法。 In order to solve the problems existing in the prior art, the present invention proposes a composite material vacuum-assisted molding system with simple structure, convenient operation, low cost and high product quality, and also provides a low process cost, strong versatility, auxiliary A vacuum-assisted molding method for composite material products with less material consumption, low process threshold, good economy, and improved product performance.

为实现上述目的,本发明提出的技术方案为一种复合材料真空辅助模压成型系统,所述系统包括一开放式成型模具,该开放式成型模具包括相对设置的上模和下模,所述下模上方密封连接有一对待成型预浸料实施真空袋压的真空袋压系统;所述开放式成型模具的外侧连接有对模具施压的模压加热系统。 In order to achieve the above object, the technical solution proposed by the present invention is a vacuum-assisted molding system for composite materials, the system includes an open forming mold, and the open forming mold includes an upper mold and a lower mold arranged oppositely, the lower mold The top of the mold is sealed and connected with a vacuum bag pressure system for applying vacuum bag pressure to the prepreg to be formed; the outside of the open molding mold is connected with a molding heating system for applying pressure to the mold.

上述的成型系统中,所述上模和下模均优选为单面模具,所述上模和下模合模后不接触、不闭合。 In the above-mentioned molding system, both the upper mold and the lower mold are preferably single-sided molds, and the upper mold and the lower mold do not contact or close after mold closing.

上述的成型系统中,所述上模的长、宽优选与拟成型制品的长、宽相同;所述下模各边缘优选超过其上放置的所述预浸料各边缘距离30mm以上。 In the above molding system, the length and width of the upper mold are preferably the same as the length and width of the product to be formed; each edge of the lower mold is preferably more than 30mm beyond each edge of the prepreg placed on it.

上述的成型系统中,所述真空袋压系统优选包括依次铺放于所述预浸料表面的隔离膜、脱模布和透气毡;所述透气毡外围连接真空袋膜,所述真空袋膜的外围通过密封连接方式包覆在下模的上表面上并形成一真空袋压腔,所述真空袋压腔通过预埋真空管与外部的真空泵连接。 In the above-mentioned molding system, the vacuum bagging system preferably includes an isolation film, a release cloth and an air felt laid on the surface of the prepreg in sequence; the outer periphery of the air felt is connected with a vacuum bag film, and the vacuum bag film The outer periphery of the lower mold is coated on the upper surface of the lower mold through a sealed connection to form a vacuum bag pressure cavity, and the vacuum bag pressure cavity is connected to an external vacuum pump through a pre-embedded vacuum tube.

作为一个总的技术构思,本发明还提供一种基于上述系统的真空辅助模压成型复合材料制品的方法,包括以下步骤: As a general technical idea, the present invention also provides a method for vacuum-assisted compression molding composite products based on the above system, including the following steps:

(1)材具准备:根据拟成型制品的工艺参数制备一包括上模和下模的开放式成型模具,并将用于成型制品的预浸料置于下模上,将隔离膜、脱模布、透气毡依次铺放在所述预浸料表面,密封连接真空袋膜形成一真空袋压腔,使真空袋压腔与外部的真空泵相连通;所述的上模和下模分别连接至一模压加热系统; (1) Material preparation: Prepare an open molding mold including an upper mold and a lower mold according to the process parameters of the product to be molded, and place the prepreg for the molded product on the lower mold, and place the isolation film, demoulding Cloth and air felt are placed on the surface of the prepreg in sequence, and the vacuum bag film is sealed and connected to form a vacuum bag pressure cavity, so that the vacuum bag pressure cavity is connected with the external vacuum pump; the upper mold and the lower mold are respectively connected to the - molding heating system;

(2)合模加压:利用所述真空泵在保持真空袋压的条件下,将所述上模和下模进行合模,通过所述模压加热系统对所述预浸料进行合模机械加压,同时通过模压加热系统对上模和下模进行加热,直至达到为所述预浸料设定的后固化周期的初始固化温度,进行合模加压下的固化处理,直至预浸料固化反应结束,最后降温、卸压,完成复合材料制品的成型。 (2) Mold clamping and pressure: use the vacuum pump to clamp the upper mold and the lower mold under the condition of maintaining the vacuum bag pressure, and perform mold clamping mechanical processing on the prepreg through the mold pressing heating system. At the same time, the upper mold and the lower mold are heated by the molding heating system until the initial curing temperature of the post-curing cycle set for the prepreg is reached, and the curing process is carried out under the clamping pressure until the prepreg is cured After the reaction is finished, the temperature is lowered and the pressure is relieved to complete the molding of the composite material product.

上述的方法中,在所述步骤(1)和步骤(2)之间优选增加一个真空袋压步骤,其具体操作方法包括:开启所述真空泵对真空袋压腔进行抽真空,达到设定的真空度后,开启所述模压加热系统加热下模,直至达到为所述预浸料设定的前固化周期的初始固化温度后,开始进行单独真空袋压下的缓慢固化,固化处理时间不超过6h。在优选的真空袋压步骤中,所述的前固化周期内可设定阶梯式固化温度,即采用逐步升温和保温的方法进行固化,但最高固化温度不超过原材料体系的固化反应最剧烈温度。所述阶梯式固化温度的范围优选为60℃~120℃。 In the above method, it is preferable to add a vacuum bag pressure step between the step (1) and the step (2). The specific operation method includes: turning on the vacuum pump to vacuum the vacuum bag pressure chamber to reach the set After the vacuum degree is reached, turn on the molding heating system to heat the lower mold until it reaches the initial curing temperature of the pre-curing cycle set for the prepreg, then start slow curing under vacuum bag pressure, and the curing treatment time does not exceed 6h. In the preferred vacuum bag pressure step, stepwise curing temperatures can be set in the pre-curing cycle, that is, curing is carried out by gradually heating up and keeping warm, but the highest curing temperature does not exceed the most intense temperature of the curing reaction of the raw material system. The range of the stepwise curing temperature is preferably 60°C to 120°C.

上述的方法中,抽真空时可通过调整所述透气毡和真空袋膜,使所述透气毡和真空袋膜与上模拟接触的部分平整无褶皱。 In the above method, during vacuuming, the air felt and the vacuum bag film can be adjusted so that the parts of the air felt and the vacuum bag film that are in contact with the upper simulation are flat and wrinkle-free.

上述的方法中,所述的后固化周期内也可设定阶梯式固化温度,温度设定范围从所述预浸料原材料体系开始反应到剧烈反应再到后固化阶段,宜采用逐步升温和保温的多步法使材料固化完全。此时,后固化周期内阶梯式固化温度的范围优选为60℃~200℃。 In the above method, the stepwise curing temperature can also be set during the post-curing period. The temperature setting range is from the beginning of the reaction of the prepreg raw material system to the violent reaction and then to the post-curing stage. Gradual heating and heat preservation should be adopted. The multi-step method makes the material fully cured. At this time, the stepwise curing temperature in the post-curing cycle is preferably in the range of 60°C to 200°C.

上述的方法中,所述真空袋压步骤和合模加压步骤中,抽真空管时的真空度均优选保持在-0.09Mpa以上。 In the above method, in the step of vacuum bag pressing and the step of clamping and pressurizing the mold, the vacuum degree when the vacuum tube is evacuated is preferably kept above -0.09Mpa.

上述的方法中,所述真空袋压系统的工作时间、开放式成型模具的合模时间以及模压加热系统的工作时间等均由可根据预浸料的固化时间进行优化和确定。根据我们反复的实验结果,所述真空袋压中的固化处理时间优选为所述合模加压中固化处理时间的0.1~0.5倍。 In the above method, the working time of the vacuum bag press system, the clamping time of the open molding mold and the working time of the molding heating system can be optimized and determined according to the curing time of the prepreg. According to our repeated experiment results, the curing treatment time in the vacuum bag pressure is preferably 0.1-0.5 times of the curing treatment time in the mold clamping pressurization.

与现有技术相比,本发明的优点在于:本发明的复合材料真空辅助模压成型系统结构简单、操作方便、成本低;采用本发明的真空辅助模压成型系统及成型方法成型的复合材料制品,不仅质量显著提高,制品内部缺陷更少,性能更好;而与传统热压罐工艺相比,本发明的成型系统及成型方法能够大大降低设备成本与制造成本,并能够获得更高的成型压力,可制备力学性能更好的复合材料制品,同时降低了安全风险。 Compared with the prior art, the present invention has the advantages of: the composite material vacuum assisted compression molding system of the present invention has simple structure, convenient operation and low cost; the composite material products formed by using the vacuum assisted compression molding system and molding method of the present invention, Not only the quality is significantly improved, the internal defects of the product are less, and the performance is better; compared with the traditional autoclave process, the molding system and molding method of the present invention can greatly reduce equipment costs and manufacturing costs, and can obtain higher molding pressure , composite products with better mechanical properties can be prepared, and safety risks are reduced at the same time.

附图说明 Description of drawings

图1为本发明中复合材料真空辅助模压成型系统的结构示意图。 Fig. 1 is a structural schematic diagram of a vacuum-assisted compression molding system for composite materials in the present invention.

图例说明:illustration:

1、上模;2、下模;3、液压机上;4、液压机下;5、预浸料;6、真空袋膜;7、透气毡;8、脱模布;9、隔离膜;10、密封胶;11、真空管;12、真空袋压腔。 1. Upper mold; 2. Lower mold; 3. Upper hydraulic press; 4. Lower hydraulic press; 5. Prepreg; 6. Vacuum bag film; 7. Air felt; 8. Release cloth; 9. Isolation film; 10. Sealant; 11. Vacuum tube; 12. Vacuum bag pressure cavity.

具体实施方式 Detailed ways

以下结合说明书附图和具体实施例对本发明作进一步的描述。 The present invention will be further described below in conjunction with the accompanying drawings and specific embodiments.

实施例:Example:

一种如图1所示的复合材料真空辅助模压成型系统,该系统包括一开放式成型模具,该开放式成型模具包括相对设置的上模1和下模2,下模2上方密封连接有一对待成型预浸料5实施真空袋压的真空袋压系统;开放式成型模具的外侧连接有对模具施压的模压加热系统(包括液压机上3和液压机下4)。本实施例中,上模1和下模2均为单面模具,上模1的长、宽与拟成型制品长、宽相同;下模2各边缘超过其上放置的预浸料5各边缘距离30mm以上。上模1和下模2合模后不接触、不闭合。 A vacuum-assisted molding system for composite materials as shown in Figure 1, the system includes an open forming mold, the open forming mold includes an upper mold 1 and a lower mold 2 arranged oppositely, and a pair of treated molds is sealed and connected above the lower mold 2 The vacuum bag pressure system for forming prepreg 5 is implemented; the outer side of the open forming mold is connected with a mold pressing heating system (including hydraulic press upper 3 and hydraulic press lower 4 ). In this embodiment, the upper mold 1 and the lower mold 2 are single-sided molds, and the length and width of the upper mold 1 are the same as the length and width of the product to be formed; the edges of the lower mold 2 exceed the edges of the prepreg 5 placed on it The distance is more than 30mm. After the upper mold 1 and the lower mold 2 are closed, they do not touch or close.

本实施例的真空袋压系统包括依次铺放于预浸料5表面的隔离膜9、脱模布8和透气毡7;透气毡7外围连接真空袋膜6,真空袋膜6的外围通过密封胶10包覆在下模2的上表面上并形成一真空袋压腔12,真空袋压腔12通过预埋的真空管11与外部的真空泵连接。 The vacuum bagging system of the present embodiment includes an isolation film 9, a release cloth 8 and an air felt 7 sequentially laid on the surface of the prepreg 5; the periphery of the air felt 7 is connected to the vacuum bag film 6, and the periphery of the vacuum bag film 6 is sealed The glue 10 is coated on the upper surface of the lower mold 2 and forms a vacuum bag pressure chamber 12 , which is connected to an external vacuum pump through a pre-embedded vacuum pipe 11 .

一种基于本实施例上述的真空辅助模压成型系统的真空辅助模压成型复合材料制品的方法,拟成型的复合材料制品为一块尺寸为250mm*250mm*2.5mm的单向碳纤维增强环氧树脂复合材料平板,其具体的成型过程包括以下步骤: A method for vacuum-assisted molding composite material products based on the above-mentioned vacuum-assisted molding system of this embodiment, the composite material product to be formed is a unidirectional carbon fiber reinforced epoxy resin composite material with a size of 250mm*250mm*2.5mm Flat plate, its specific molding process includes the following steps:

(1)材具准备:按以下规格和要求准备原材料: (1) Material preparation: Prepare raw materials according to the following specifications and requirements:

增强体:T700SC碳纤维; Reinforcement: T700SC carbon fiber;

树脂体系:环氧树脂TDE-85、酸酐THPA、促进剂DMP-30按100∶100∶0.9配制而成; Resin system: Epoxy resin TDE-85, anhydride THPA, accelerator DMP-30 prepared according to 100:100:0.9;

预浸料:碳纤维与树脂体系经缠绕机缠绕制得; Prepreg: Carbon fiber and resin system are wound by winding machine;

隔离膜:耐高温聚乙烯薄膜; Isolation film: high temperature resistant polyethylene film;

脱模布:耐高温白色编织布; Release cloth: high temperature resistant white woven cloth;

透气毡:采用具有优良透气性能和耐压性能的聚酯透气毡; Air felt: Polyester air felt with excellent air permeability and pressure resistance;

真空袋膜:采用优良耐温性能的尼龙薄膜; Vacuum bag film: nylon film with excellent temperature resistance;

排气通道:采用60目的编织网格布; Exhaust channel: 60-mesh woven mesh cloth is used;

密封胶:耐高温压敏密封胶带。 Sealant: high temperature resistant pressure sensitive sealing tape.

(2)材料铺放:如图1所示,裁剪250mm×250mm的预浸料5六块,0°铺层于下模2的上表面上;准备250mm×250mm的隔离膜9两块,铺设于预浸料5的表面;280mm×280mm脱模布8一块,铺设于隔离膜9上;280mm×360mm透气毡7一块,铺设于脱模布8上;400mm×450mm真空袋膜6一块,透气毡7的外围上方连接真空袋膜6,真空袋膜6的外围通过密封胶10包覆在下模2的上表面上并形成一真空袋压腔12,真空袋压腔12通过预埋真空管11与外部的真空泵连接。 (2) Material placement: As shown in Figure 1, cut 5 and six pieces of prepregs with a size of 250mm×250mm, and lay them on the upper surface of the lower mold 2 at 0°; prepare two pieces of 9 isolation films with a size of 250mm×250mm, and lay On the surface of prepreg 5; 8 pieces of 280mm×280mm release cloth, laid on the isolation film 9; 7 pieces of 280mm×360mm air felt, laid on the release cloth 8; 6 pieces of 400mm×450mm vacuum bag film, breathable A vacuum bag film 6 is connected above the periphery of the felt 7, and the periphery of the vacuum bag film 6 is coated on the upper surface of the lower mold 2 by a sealant 10 to form a vacuum bag pressure chamber 12, which is connected by a pre-embedded vacuum tube 11 and External vacuum pump connection.

(3)真空袋压:开启真空泵对真空袋压腔12进行抽真空,抽真空时调整透气毡7和真空袋膜6,使透气毡7和真空袋膜6与上模1拟接触的部分平整无褶皱;使真空度达到设定的-0.09MPa以上时,开启模压加热系统加热下模2,直至达到为预浸料设定的前固化周期的初始固化温度85℃后,开始进行单独真空袋压下的缓慢固化处理,处理时间为1小时。 (3) Vacuum bag pressure: Turn on the vacuum pump to evacuate the pressure chamber 12 of the vacuum bag, adjust the air felt 7 and the vacuum bag film 6 during vacuuming, so that the part of the air felt 7 and the vacuum bag film 6 in contact with the upper mold 1 is flat No wrinkles; when the vacuum degree reaches the set value above -0.09MPa, turn on the molding heating system to heat the lower mold 2 until it reaches the initial curing temperature of 85°C in the pre-curing cycle set for the prepreg, and then start a separate vacuum bag Slow curing treatment by pressing, the treatment time is 1 hour.

(4)合模加压:上述步骤(3)完成后,利用模压加热系统的液压机上3和液压机下4将上模1和下模2进行合模,在保持真空袋压(-0.09MPa)的条件下通过模压加热系统对预浸料进行合模机械加压至0.5MPa,在该温度(85℃)及压力条件下继续固化3h,继续保持真空度(-0.09MPa)和外压(0.5MPa),再通过模压加热系统对上模1和下模2进行加热并升温,升温速率为3℃/min,直至达到为预浸料5设定的后固化周期的初始固化温度120℃,继续进行合模加压下的固化处理(真空负压-0.09MPa,模压压力0.5MPa,120℃),保温时间为4h,最后保压至成型系统自然冷却至室温、卸压,完成复合材料制品的成型。 (4) Mold clamping and pressurization: After the above step (3) is completed, use the hydraulic press upper 3 and hydraulic press lower 4 of the molding heating system to clamp the upper mold 1 and the lower mold 2, while maintaining the vacuum bag pressure (-0.09MPa) Under certain conditions, the prepreg is mechanically pressurized to 0.5MPa through the molding heating system, and continues to cure for 3 hours at this temperature (85°C) and pressure, and continues to maintain vacuum (-0.09MPa) and external pressure (0.5 MPa), then the upper mold 1 and the lower mold 2 are heated and heated by the molding heating system at a heating rate of 3°C/min until the initial curing temperature of 120°C in the post-curing cycle set for prepreg 5 is reached, continue Carry out curing treatment under mold clamping pressure (vacuum negative pressure -0.09MPa, molding pressure 0.5MPa, 120°C), holding time is 4h, and finally keep the pressure until the molding system is naturally cooled to room temperature, and the pressure is released to complete the composite product. forming.

经检验,本实施例制得的单向碳纤维增强环氧树脂复合材料平板纤维体积含量70%以上,孔隙率低于0.5%,厚度均匀,外观质量良好。 After inspection, the unidirectional carbon fiber-reinforced epoxy resin composite plate prepared in this example has a fiber volume content of more than 70%, a porosity of less than 0.5%, uniform thickness, and good appearance quality.

Claims (10)

1. composite vacuum aided compression molding system; It is characterized in that: said formation system comprises an open mould; This open mould comprises the upper die and lower die that are oppositely arranged, and said counterdie top is sealedly connected with a pair of prepreg to be formed and implements the vacuum bag pressing system that vacuum bag is pressed; The outside of said open mould is connected with the mold pressing heating system that mould is exerted pressure.
2. formation system according to claim 1 is characterized in that: said upper die and lower die are one-side mould, do not contact behind the said upper die and lower die matched moulds, not closed.
3. formation system according to claim 2 is characterized in that: the length and width of said patrix is identical with the length and width of intending moulded products; Each edge of said counterdie surpass its said prepreg of going up placement each more than the Edge Distance 30mm.
4. according to each described formation system in the claim 1~3, it is characterized in that: said vacuum bag pressing system comprises that lay is in barrier film, release cloth and the airfelt on said prepreg surface successively; The peripheral vacuum bag film that connects of said airfelt, the periphery of said vacuum bag film are coated on the upper surface of counterdie and form a vacuum bag through the mode of being tightly connected presses the chamber, and said vacuum bag presses the chamber to be connected through the vavuum pump of pre-buried vacuum tube with the outside.
5. method like arbitrary said formation system vacuum aided compression molding composite product in the claim 1~4 may further comprise the steps:
(1) the material tool is prepared: the open mould that comprises upper die and lower die according to the technological parameter preparation one of intending moulded products; And the prepreg that will be used for moulded products places counterdie; Barrier film, release cloth, airfelt are laid in said prepreg surface successively; The vacuum bag film that is tightly connected forms a vacuum bag and presses the chamber, makes vacuum bag press the chamber to be connected with outside vavuum pump; Described upper die and lower die are connected to a mold pressing heating system respectively;
(2) matched moulds pressurization: utilize said vavuum pump under the condition that keeps vacuum bag to press; Said upper die and lower die are carried out matched moulds; Through said mold pressing heating system said prepreg is carried out the pressurization of matched moulds machinery, through the mold pressing heating system upper die and lower die are heated simultaneously, until the initial solidification temperature of the back cure cycle that is reached for said prepreg setting; Carry out matched moulds and add the cured of depressing; Finish until the prepreg curing reaction, the moulding of composite product is accomplished in cooling, release at last.
6. method according to claim 5; It is characterized in that; Between said step (1) and step (2), increase a vacuum bag and press step, its concrete operation method comprises: open said vavuum pump and press the chamber to vacuumize to vacuum bag, after vacuum bag is pressed and reached the vacuum of setting; Open said mold pressing heating system heating counterdie; After the initial solidification temperature of the preceding cure cycle that is reached for said prepreg setting, begin to carry out the slow curing that independent vacuum bag is depressed, the cured time is no more than 6h.
7. method according to claim 6; It is characterized in that; Set the staged solidification temperature before described in the cure cycle; Promptly adopt the method that progressively heats up and be incubated to be cured, but the highest solidification temperature is no more than the most violent temperature of curing reaction of said prepreg raw material system, the scope of said staged solidification temperature is 60 ℃~120 ℃.
8. method according to claim 6 is characterized in that: the cured time during said vacuum bag is pressed is 0.1~0.5 times of cured time in the said matched moulds pressurization.
9. according to each described method in the claim 5~8; It is characterized in that: set the staged solidification temperature in the cure cycle of described back; Promptly adopt the method that progressively heats up and be incubated to be cured, the scope of staged solidification temperature is 60 ℃~200 ℃ in the cure cycle of said back.
10. according to each described method in the claim 5~8, it is characterized in that: the vacuum when said vacuum bag is pressed remains on-more than the 0.09Mpa.
CN2012102425007A 2012-07-13 2012-07-13 Vacuum assisted molding system of composite and molding method of composite Pending CN102765198A (en)

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Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101003179A (en) * 2007-01-12 2007-07-25 连云港中复连众复合材料集团有限公司 Method for manufacturing blades of large-scale wind driven generator
CN101143492A (en) * 2007-11-02 2008-03-19 贵州云马飞机制造厂 Compression type RTM forming method
CN101704300A (en) * 2009-11-12 2010-05-12 江苏九鼎新材料股份有限公司 Integral one-step molding technique of wind power blade
CN102431184A (en) * 2011-10-21 2012-05-02 中国兵器工业集团第五三研究所 Technological method for forming multiple composite plates in one step

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101003179A (en) * 2007-01-12 2007-07-25 连云港中复连众复合材料集团有限公司 Method for manufacturing blades of large-scale wind driven generator
CN101143492A (en) * 2007-11-02 2008-03-19 贵州云马飞机制造厂 Compression type RTM forming method
CN101704300A (en) * 2009-11-12 2010-05-12 江苏九鼎新材料股份有限公司 Integral one-step molding technique of wind power blade
CN102431184A (en) * 2011-10-21 2012-05-02 中国兵器工业集团第五三研究所 Technological method for forming multiple composite plates in one step

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JP7389193B2 (en) 2021-08-27 2023-11-29 臺灣塑膠工業股▲ふん▼有限公司 Composite material molding method
EP4140713B1 (en) * 2021-08-27 2024-10-09 Formosa Plastics Corporation Composite material and method for molding composite material
US12122107B2 (en) 2021-08-27 2024-10-22 Formosa Plastics Corporation Composite material and method for molding composite material
CN114454514A (en) * 2022-01-28 2022-05-10 株洲博雅科技股份有限公司 A busbar hot pressing process and hot pressing equipment
CN114750428A (en) * 2022-03-14 2022-07-15 上海喆航航空科技有限公司 Vacuum forming preparation method of helicopter body composite material
CN115071164A (en) * 2022-06-23 2022-09-20 廊坊市飞泽复合材料科技有限公司 A composite material pressurized prepreg molding die and molding method
CN115302811A (en) * 2022-06-29 2022-11-08 中航西安飞机工业集团股份有限公司 Forming device and forming method for U-shaped sandwich front edge
CN115352092A (en) * 2022-07-22 2022-11-18 南京玻璃纤维研究设计院有限公司 An automatic vacuum bagging method in the forming process of composite material sheet

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Application publication date: 20121107